Problem 3.17. Torsion of open and closed section cantilever

A cantilever beam (L = 2.5 m) is subjected to t  = 4 kNm/m uniformly distributed torque. Calculate the rotation at the free end in the
case of open and closed rectangular hollow sections (see Figures a) and b)). Thickness of the wall is t = 8 mm, width and height of the cross section are h = 200 mm. The material properties are E = 200 GPa = 100 × 103 N/mm2, G = 80.8 GPa = 80.8 × 103 N/mm2.
(Neglect restrained warping.)

Solve Problem

Solve

Rotation of the closed section beam, ψ=

Rotation of the open section beam, ψ=

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Steps

Step by step

Step 1. Calculate the torsional stiffnesses of cross sections a) and b)

Check torsional stiffness of the closed section

Eq.(3-111)
GIt,closed=4Ac21Gtds=4ht44htGt=20083×8×80.8×103=4.575×1012 Nmm2=4575 kNm2

Check torsional stiffness of the open section

Eq.(3-100)
GIt,open=Gk=14bktk33=G4htt33=80.8×10342008833=1.059×1010Nmm2=10.59 kNm2

Step 2. Draw the torque diagram and the rate of twist distribution along the length of the beam.

Check diagrams

Step 3. Determine the rotation of the beam end.

Check rotation

Rotation is obtained by the integration of the rate of twist function along the beam’s length. The rotation of the beam end results in the area of the rate of twist diagram.

See geometrical equation in Table 3.7.

ϑ=dψdx     ψ=0Lϑdx=ϑL2=tL22GIt

for closed section beam

ψclosed=tL22GIt,closed=4×2.522×4575=0.00273

for open section beam

ψopen=tL22GIt,open=4×2.522×10.59=1.18

Results

Show worked out solution

The torsional stiffnesses of the closed cross section is

Eq.(3-111)
GIt,closed=4Ac21Gtds=4ht44htGt=20083×8×80.8×103=4.575×1012 Nmm2=4575 kNm2

The torsional stiffnesses of the open cross section is

Eq.(3-100)
GIt,open=Gk=14bktk33=G4htt33=80.8×10342008833=1.059×1010Nmm2=10.59 kNm2

From uniformly distributed torque load the internal force diagram and the rate of twist distribution is linear along the length of the beam:

Rotation is obtained by the integration of the rate of twist function along the beam’s length. The rotation of the beam end results in the area of the rate of twist diagram.

See geometrical equation in Table 3.7.

 

ϑ=dψdx     ψ=0Lϑdx=ϑL2=tL22GIt

for closed section beam

ψclosed=tL22GIt,closed=4×2.522×4575=0.00273

for open section beam

ψopen=tL22GIt,open=4×2.522×10.59=1.18